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ENGINEERING PREDICATION OF TURBULENT SKIN FRICTION AND HEAT TRANSFER IN HIGH-SPEED FLOW.

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BookPublisher: Nasa, Washington, D.C. 1974Description: 86.DDC classification: NASA | TN D-7507

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Item type	Current location	Collection	Call number	Status	Date due	Barcode	Item holds
Technical Report	PK Kelkar Library, IIT Kanpur	General Stacks	NASA TN D-7507 (Browse shelf)	Not for loan		TR11586

Total holds: 0

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Previous	NASA TN D-7504 COMPUTER PROGRAM FOR PRESSURIZATION (RAMP) AND PRESSURIZED EXPULISION FROM A CRYOGENIC LIQUID PROPELLANT TANK.	NASA TN D7505 EFFECT OF CANARD LOCATION AND AERODYNAMIC-CENTER SHIPTS RELATED TO MANEUVERING AIRCRAFT AT TRANSONIC SPEEDS.	NASA TN D-7506 PRESSURE MEASUREMENTS ON THE LEADING EDGE OF A SWEFT WING AT MATCH 2.2	NASA TN D-7507 ENGINEERING PREDICATION OF TURBULENT SKIN FRICTION AND HEAT TRANSFER IN HIGH-SPEED FLOW.	NASA TN D-7508 A NEW TECHNIQUE FOR CALCULATING REENTRY BASE HEATING.	NASA TN D-7509 EN ROUTE POSITION AND TIME CONTROL OF AIRCRAFT USING KALAMAN FILTERING OF RADIO AID DATA.	NASA TN D-7510 COMPARISON OF MEASURED AND CALCULATED VELOCITY PROFILES OF A LAMINAR INCOMPRESSIBLE FREE JET AT LOW REYNOLDS NUMBERS.	Next

Bound With Nasa Tn D 7500-7506,7508-10.Lack No-7503.

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